Sealing arrangement for sealing a gap between two components which can rotate in relation to each other about a common rotational axis

Inactive Publication Date: 2006-06-22
MTU AERO ENGINES GMBH +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0008] It is now possible, in a surprisingly simple way, to adjust the gap between the two components and thereby to control the sealing action of the brush seal fitted between the two components.
[0009] The sealing arrangement according to the invention leads to significant advantages.
[0010] For example, the axial displaceability of the first component allows optimum adjustment of the brush seal during initial installation. Moreover, the configuration of the sealing arrangement according to the invention ensures simplified fitting of the brush seal.
[0011] Furthermore, in the event of wear to the brush s

Problems solved by technology

It is known that a brush seal of this type cannot be designed with a large coverage, since otherwise the driving losses and the resultant generation of heat increase correspondingly.
This proves disadvantageous since accurate production is known to be associated with high production costs.
A further drawback of the known brush seals is that in the event of a drop in the sealing action of the brush seal it is necessary t

Method used

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  • Sealing arrangement for sealing a gap between two components which can rotate in relation to each other about a common rotational axis
  • Sealing arrangement for sealing a gap between two components which can rotate in relation to each other about a common rotational axis
  • Sealing arrangement for sealing a gap between two components which can rotate in relation to each other about a common rotational axis

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Embodiment Construction

[0018] A sealing arrangement, which is denoted overall by reference numeral 10 in FIG. 1, for sealing a gap between two components which can move rotationally with respect to one another in a turbomachine (not shown in more detail), such as for example a steam turbine or a gas turbine, comprises a first component 12, which is surrounded by a casing 14, and a second component 16. The two components 12, 16 have a common axis of rotation 18.

[0019] The second component 16 is mounted such that it can move in rotation with respect to the first component 12 about the axis of rotation 18. The rotational mobility of the second component 16 is indicated by arrow 20.

[0020] A brush seal 22 has been introduced into the annular gap between the components 12, 16, in order, for example, to seal off a region 24 which is at a high pressure with respect to a region 26 which is at a lower pressure.

[0021] The brush seal 22 in this case comprises a brush casing 28 and a plurality of bristles 30 fitted...

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PUM

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Abstract

A sealing arrangement for sealing a gap between two components which can move rotationally with respect to one another about a common axis of rotation, having a brush seal on a first component which interacts with a sealing surface of the second component. The sealing surface is conical in form, with at least one component being axially displaceable and adjustable with respect to the other component in order to reduce the gap between the brush seal and the second component.

Description

[0001] This application claims the priority of German application no. 10227630.7, filed Jun. 21, 2002, and PCT International Patent Application No. PCT / DE03 / 01973, filed Jun. 13, 2003, the disclosure of which is expressly incorporated by reference herein.BACKGROUND AND SUMMARY OF THE INVENTION [0002] The invention relates to a sealing arrangement for sealing a gap between two components which can move rotationally with respect to one another about a common axis of rotation. [0003] The use of brush seals for sealing two components which can move rotationally with respect to one another is well known. The brush seal in this case substantially comprises a brush casing, which is mounted in the first component, and a plurality of bristles which have been introduced into the brush casing and the free ends of which are directed onto a sealing surface of the second component. In particular in turbomachines, such as for example steam turbines or gas turbines, brush seals are used to seal an ...

Claims

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Application Information

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IPC IPC(8): F16J15/44F16J15/22F16J15/32
CPCF16J15/3288
Inventor BEICHL, STEFANRAUSCHMEIER, ALEXANDER
Owner MTU AERO ENGINES GMBH
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